Mooney M20K - General; Skin Specifications

MOONEY
AIRCRAFT
CORPORATION
M20K
SERVICE
AND
MAINTENANCE
MANUAL
20-00-00
-GENERAL
Alteration
and
Sub
Parts
A,
D
and
E
of
FAR
65.
Cer-
tification.
Advisory
Circular
43.13-1()
outlines
inspec-
This
chapter
of
the
manual
discusses
treatment
of
tion
and
repair
practices
acceptable
to
the
F.A.A.
Ad-
metal
surfaces
for
corrosion
control
and
the
identifica-
ministrator.
tion
of
skin
panels
for
replacement
purposes.
Those
who
inspect
or
repair
aircraft
should
consult
FAR
43,
20-00´•01
SKIN
SPECIFICATIONS
Maintenance,
Preventive
Maintenance,
Rebuilding
and
STA
STA
STA
STPI
STA
210,97
147.75
103.50
59~25
24,50
STA
193.50
5
1
r4
I
r3
I r2
18
15
19
13
12
17
i
11
10
i
14
-J
L9
WING
SKIN
PANELS
WING
SKIN
PANELS
FIGURE
20
1
INDEX
SKIN
.MATERIAL
INDEX
SKIN
MATERIAL
NO.
THICKNESS
NO.
.THICKNESS
1.
0.063
2024
T-3
CLAD
12. 0.025(c)
2024
T-3
CLAD
2.
0.050
2024
T-3
CLAD
13.
0.020(a)
2024
T-3
CLAD
3.
0.040
2024
T-3
CLAD
14.
0.032
2024
T-3
CLAD
4.
0.032
2024
T-3
CLAD
15.
0.040(b)
2024
T-3
CLAD
5.
0.025
2024
T-3
CLAD
16.
0.040(d)
2024
T-3
CLAD
6.
0.025
20241-3
CLAD
17.
o.ols(a)
2024
T-3
CLAD
7.
0.032
2024
T-3
CLAD
18- 0.050(b)
2024
T-3
CLAD
8.
0.040
2024
T-3
CLAD
19-
Polyester
Glass-Fiber
Reinforced
9.
0.025
20241-3
CLAD
10.
0.025
2024
T-3
CLAD
11.
0.025
2024
T-3
CLAD
(a)
Same
thickness
on
top
and
bottom.
(b) Top
of
wing
only.
(c)
Top
aft
flap
skin
that
section).
(d) Top
inboard
flap
skin.
20-00-00
OLDWILLWAYNE